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US4847964A - Method of producing a crown for an articulated piston - Google Patents

Method of producing a crown for an articulated piston Download PDF

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Publication number
US4847964A
US4847964A US07/261,457 US26145788A US4847964A US 4847964 A US4847964 A US 4847964A US 26145788 A US26145788 A US 26145788A US 4847964 A US4847964 A US 4847964A
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US
United States
Prior art keywords
crown
side wall
machining
top face
rough
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US07/261,457
Inventor
Marshal Adams
Jerry M. Lechner
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Caterpillar Inc
Original Assignee
Caterpillar Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Caterpillar Inc filed Critical Caterpillar Inc
Assigned to CATERPILLAR INC. reassignment CATERPILLAR INC. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: ADAMS, MARSHAL, LECHNER, JERRY M.
Priority to US07261457 priority Critical patent/US4847964B1/en
Priority to DE8989901407T priority patent/DE3875253T2/en
Priority to JP1501366A priority patent/JP2801049B2/en
Priority to EP89901407A priority patent/EP0439459B1/en
Priority to PCT/US1988/004605 priority patent/WO1990004491A1/en
Priority to BR888807924A priority patent/BR8807924A/en
Publication of US4847964A publication Critical patent/US4847964A/en
Application granted granted Critical
Publication of US4847964B1 publication Critical patent/US4847964B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/10—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass pistons
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00—Pistons 
    • F02F3/0015—Multi-part pistons
    • F02F3/0069—Multi-part pistons the crown and skirt being interconnected by the gudgeon pin
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/49249—Piston making
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/49249—Piston making
    • Y10T29/49252—Multi-element piston making
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/49249—Piston making
    • Y10T29/49265—Ring groove forming or finishing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/4998—Combined manufacture including applying or shaping of fluent material
    • Y10T29/49988—Metal casting
    • Y10T29/49989—Followed by cutting or removing material
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49995—Shaping one-piece blank by removing material
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49995—Shaping one-piece blank by removing material
    • Y10T29/49996—Successive distinct removal operations

Definitions

  • This invention relates to a method of producing a crown of a two piece piston and more specifically to the method of machining the finished crown.
  • Such increase in pressures have required the improvement of the integrity of the piston to withstand the increased stresses therein.
  • pistons are made of aluminum or cast iron.
  • the piston described herein meets the requirement to withstand the increased pressures by providing a crown of a two piece articulated piston that is machined from a forging.
  • the material of the forging is SAE4140, which is an alloy steel containing chrome and molybdenum.
  • the material was found to be extremely difficult to machine. Since the material is extremely tough, it has the characteristic of causing gumming of the tooling, and it was necessary to develop a unique machining method which is the subject of this invention.
  • the method of producing a crown of an articulated piston has a circular top face, a combustion crater extending from and below the top face, a sidewall depending from the top face which has a cylindrical surface.
  • a plurality of ring grooves on the sidewall are provided, which are disposed at spaced locations below the top face.
  • the sidewall has an inner surface forming a first side of a cooling gallery that extends adjacent to top face and the combustion crater.
  • a depending center section has a lateral extending pin-receiving bore, therethrough, and a surface adjacent to the crater forming a second wall of the cooling gallery.
  • the sidewall has a bottom face extending between the center of the sidewall and the cooling gallery and is disposed above the pin receiving bore.
  • the machining steps are as follows: the entire outer surface of the sidewall, the ring grooves, the top face, and the combustion crater are rough machined.
  • the next step is finish machining of the bottom face of the crown.
  • the crown is then removed from the holding device and a chuck member is inserted through the pin receiving bore.
  • the crown is then positioned with the bottom face against a stop and the one side of the cooling gallery against a locator. This positions the crown for the finishing operation which includes finish machining the combustion crater, the top face, the ring grooves, and the cylindrical outer surface of the sidewall while the crown is so positioned.
  • a second aspect of the invention is a method of the rough machining wherein one portion of the outer surface is grasped in a chuck and the rough machining of that surface proceeds along the outer surface, ending in an area overlying the position of one of the ring grooves.
  • the crown is then removed from the chuck, reinserted on the machined surface, and the remaining material is removed from the outer surface, following which the ring groove is then machined, removing the juncture at the interrupted cut.
  • FIG. 1 is a cross sectional view of a two piece articulated piston wherein the crown is shown in section and the skirt, rod and piston pin are shown in broken lines.
  • FIG. 2 is a schematic diagram of the method steps producing a crown for a two piece articulated piston.
  • FIG. 1 a two piece articulated piston 10 is illustrated.
  • the two piece piston includes a crown 11 shown in section and an appending skirt 12 shown in broken lines.
  • the crown and skirt are attached to a connecting rod 14 by a piston pin 16.
  • the connecting rod 14 is in turn attached to a crankshaft of an engine not shown.
  • the crown 11 has a circular top face 18 and a combustion crater 20 extending from and below the top face 18.
  • a circular sidewall 22 depends downwardly from the top face 18 and has a cylindrical outer surface 24.
  • a plurality of ring grooves 26 extend from the cylindrical outer surface 24 into the sidewall 22 and are disposed at spaced locations below the top face 18.
  • the sidewall 22 has an inner surface 28 forming a first side of an internal cooling gallery 30. Drain passages 27 extend from the bottom of the lower ring groove 29 into the cooling gallery 30.
  • the inner surface 28 extends upwardly to adjacent the top face 18 and the combustion crater 20.
  • a depending center section 32 extends downwardly from below and adjacent to the combustion crater 20 and the top face 18 defining a pair of bosses 34.
  • Each boss has a pin receiving bore 36 therethrough and being in line constitute a continuous pin bore for receiving the piston pin 36.
  • Bushings 37 are pressed into the pin receiving bore.
  • a second side 38 of the cooling gallery 30 is provided by a surface of the center section 32 that begins below the top face 18 and adjacent to the combustion crater 20.
  • the sidewall 22 has a bottom face 40 extending between the cylindrical surface 24 and the cooling gallery 30.
  • the surface of the bottom face 40 is located above the pin bore 36 or more specifically above a horizontal plane that is tangent to the upper circular surface of the pin bore.
  • the first step of producing the crown described above is the forging of a billet of an steel alloy material consisting of a chrome molybdenum alloy.
  • This material is the composition set forth in SAE4041 alloy steel. It is composed of carbon, manganese, phosphorus, sulfur, silicon, chromium, molybdenum, and the balance iron and trace elements.
  • the billet is then placed in a press and is forged by a die into the approximate shape of the piston crown wherein sufficient material is provided to allow for the two step machining process described below.
  • the first step includes positioning the crown by chucking it in a lathe or a machining center on its bosses, leaving the outer surface of the sidewall clear for machining.
  • the crown is then rough machined producing the top face 18, the crater 20, the cylindrical outer surface of the side wall and the ring grooves.
  • the drain passages for an oil ring in the lower ring groove may also be drilled during this step.
  • An alternate method for the first step is to chuck on the forged outer surface of the sidewall and rough machine one portion thereof, interrupting the cut on the outer cylindrical surface 24 in an area overlying one of the ring grooves.
  • the crown is then removed from the chuck and rechucked on the rough machined surface.
  • the remaining surfaces described above are then rough machined, again interrupting the cut on the cylindrical sidewall in the area overlying the one ring groove, following which a rough cut is made cutting the ring grooves and in this manner removing any juncture of the machine surface caused by the interrupted cut.
  • the crown is chucked on the outer cylindrical surface, exposing the lower surface of the piston for machining.
  • the bottom face 40 and the walls of the cooling gallery 30 are machined as are the pin bores 36 in the bosses 34.
  • a bar or chuck member is inserted into the pin bores, which is grasped by a drawbar within the machine chuck.
  • the bottom face 40 of the piston crown is drawn against a face plate or locator of the chuck. This locates the crown in a centered position on the chuck for the final machining operation.
  • the crater surface, the top face surface, the cylindrical outer surface, and the ring grooves are then finish machined.
  • the crown may be removed from the chuck and prepared for final assembly.
  • the two step machining of the crater, top face, cylindrical outer surface and the ring grooves produces a finished surface free of tool marks or other infractions that may propagate any cracks that will destroy the integrity of the crown.
  • the above method does not include the processing steps to produce the finished cooling gallery or the steps for the forging process.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)
  • Forging (AREA)

Abstract

A method of producing a steel alloy articulate piston crown from a forging including the steps of rough machining a combustion crater, a top face, a plurality of ring grooves and a bottom face, chucking on a member inserted into a pin receiving bore, drawing the crown's bottom face against a stop and one side of a cooling gallery against a locator, and finish machining the combustion crater, the top face, and the plurality of ring grooves.

Description

TECHNICAL FIELD
This invention relates to a method of producing a crown of a two piece piston and more specifically to the method of machining the finished crown.
BACKGROUND
The development of engines over the past few years have included increasing the horsepower without increasing the displacement of the engine. To obtain this increased horsepower, it has been necessary to increase the combustion pressures of the combustion chamber which are transferred through the piston into the connecting rod.
Such increase in pressures have required the improvement of the integrity of the piston to withstand the increased stresses therein. In the past and in many cases today, such pistons are made of aluminum or cast iron. The piston described herein meets the requirement to withstand the increased pressures by providing a crown of a two piece articulated piston that is machined from a forging. The material of the forging is SAE4140, which is an alloy steel containing chrome and molybdenum.
During the development of the higher grade steel piston crown, the material was found to be extremely difficult to machine. Since the material is extremely tough, it has the characteristic of causing gumming of the tooling, and it was necessary to develop a unique machining method which is the subject of this invention.
DISCLOSURE OF THE INVENTION
In one aspect of the invention, the method of producing a crown of an articulated piston is provided. The crown has a circular top face, a combustion crater extending from and below the top face, a sidewall depending from the top face which has a cylindrical surface. A plurality of ring grooves on the sidewall are provided, which are disposed at spaced locations below the top face. The sidewall has an inner surface forming a first side of a cooling gallery that extends adjacent to top face and the combustion crater. A depending center section has a lateral extending pin-receiving bore, therethrough, and a surface adjacent to the crater forming a second wall of the cooling gallery. The sidewall has a bottom face extending between the center of the sidewall and the cooling gallery and is disposed above the pin receiving bore.
The machining steps are as follows: the entire outer surface of the sidewall, the ring grooves, the top face, and the combustion crater are rough machined. The next step is finish machining of the bottom face of the crown. The crown is then removed from the holding device and a chuck member is inserted through the pin receiving bore. The crown is then positioned with the bottom face against a stop and the one side of the cooling gallery against a locator. This positions the crown for the finishing operation which includes finish machining the combustion crater, the top face, the ring grooves, and the cylindrical outer surface of the sidewall while the crown is so positioned.
A second aspect of the invention is a method of the rough machining wherein one portion of the outer surface is grasped in a chuck and the rough machining of that surface proceeds along the outer surface, ending in an area overlying the position of one of the ring grooves. The crown is then removed from the chuck, reinserted on the machined surface, and the remaining material is removed from the outer surface, following which the ring groove is then machined, removing the juncture at the interrupted cut.
The foregoing and other aspects will become apparent from the following description when considered in conjunction with the accompanying drawings. It is especially understood that the drawings are not intended as a definition of the invention, but are for the purpose of illustration only.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a cross sectional view of a two piece articulated piston wherein the crown is shown in section and the skirt, rod and piston pin are shown in broken lines.
FIG. 2 is a schematic diagram of the method steps producing a crown for a two piece articulated piston.
BEST MODE FOR CARRYING OUT THE INVENTION
In FIG. 1, a two piece articulated piston 10 is illustrated. The two piece piston includes a crown 11 shown in section and an appending skirt 12 shown in broken lines. The crown and skirt are attached to a connecting rod 14 by a piston pin 16. The connecting rod 14 is in turn attached to a crankshaft of an engine not shown.
The crown 11 has a circular top face 18 and a combustion crater 20 extending from and below the top face 18. A circular sidewall 22 depends downwardly from the top face 18 and has a cylindrical outer surface 24. A plurality of ring grooves 26 extend from the cylindrical outer surface 24 into the sidewall 22 and are disposed at spaced locations below the top face 18.
The sidewall 22 has an inner surface 28 forming a first side of an internal cooling gallery 30. Drain passages 27 extend from the bottom of the lower ring groove 29 into the cooling gallery 30. The inner surface 28 extends upwardly to adjacent the top face 18 and the combustion crater 20. A depending center section 32 extends downwardly from below and adjacent to the combustion crater 20 and the top face 18 defining a pair of bosses 34. Each boss has a pin receiving bore 36 therethrough and being in line constitute a continuous pin bore for receiving the piston pin 36. Bushings 37 are pressed into the pin receiving bore. A second side 38 of the cooling gallery 30 is provided by a surface of the center section 32 that begins below the top face 18 and adjacent to the combustion crater 20.
The sidewall 22 has a bottom face 40 extending between the cylindrical surface 24 and the cooling gallery 30. The surface of the bottom face 40 is located above the pin bore 36 or more specifically above a horizontal plane that is tangent to the upper circular surface of the pin bore.
Referring now to FIG. 2, the first step of producing the crown described above is the forging of a billet of an steel alloy material consisting of a chrome molybdenum alloy. This material is the composition set forth in SAE4041 alloy steel. It is composed of carbon, manganese, phosphorus, sulfur, silicon, chromium, molybdenum, and the balance iron and trace elements.
The billet is then placed in a press and is forged by a die into the approximate shape of the piston crown wherein sufficient material is provided to allow for the two step machining process described below.
In one aspect of the invention, the first step includes positioning the crown by chucking it in a lathe or a machining center on its bosses, leaving the outer surface of the sidewall clear for machining. In this step, the crown is then rough machined producing the top face 18, the crater 20, the cylindrical outer surface of the side wall and the ring grooves. The drain passages for an oil ring in the lower ring groove may also be drilled during this step.
An alternate method for the first step is to chuck on the forged outer surface of the sidewall and rough machine one portion thereof, interrupting the cut on the outer cylindrical surface 24 in an area overlying one of the ring grooves. The crown is then removed from the chuck and rechucked on the rough machined surface. The remaining surfaces described above are then rough machined, again interrupting the cut on the cylindrical sidewall in the area overlying the one ring groove, following which a rough cut is made cutting the ring grooves and in this manner removing any juncture of the machine surface caused by the interrupted cut.
During the rough machining operation, approximately 0.030 inch (0.75 mm) of material is left for the finish machining operation.
In the next step, the crown is chucked on the outer cylindrical surface, exposing the lower surface of the piston for machining. In this step, the bottom face 40 and the walls of the cooling gallery 30 are machined as are the pin bores 36 in the bosses 34.
The next step in the bushings 37 are pressed into the pin bores 36 which are then finish machined to the dimension which will be acceptable to the piston pin when installed in the engine.
In the following step, a bar or chuck member is inserted into the pin bores, which is grasped by a drawbar within the machine chuck. The bottom face 40 of the piston crown is drawn against a face plate or locator of the chuck. This locates the crown in a centered position on the chuck for the final machining operation. The crater surface, the top face surface, the cylindrical outer surface, and the ring grooves are then finish machined.
Following the finish machining operation, the crown may be removed from the chuck and prepared for final assembly.
The two step machining of the crater, top face, cylindrical outer surface and the ring grooves produces a finished surface free of tool marks or other infractions that may propagate any cracks that will destroy the integrity of the crown.
The above method does not include the processing steps to produce the finished cooling gallery or the steps for the forging process.
Other aspects, objects, and advantages become apparent from study of the specification, drawings, and appended claims.

Claims (9)

We claim:
1. A method of producing a crown of an articulated piston, the crown having a circular top face, a combustion crater extending from and below the top face, a side wall depending from the top face and having a cylindrical outer surface, a plurality of ring grooves in the side wall and disposed at spaced locations below the top face, the side wall having an inner surface forming a first side of a cooling gallery that extends adjacent the top face and the combustion crater, a depending center section having a laterally-extending pin-receiving bore therethrough, said center section having a surface forming a second side of the cooling gallery, the side wall having a bottom face extending between the cylindrical side wall and the cooling gallery and disposed above the pin-receiving bore; the method comprising the steps of:
a. rough machining the cylindrical outer surface of the side wall, the ring grooves, the top face, and the combustion crater;
b. finish machining the bottom face of the crown;
c. inserting a member through the pin-receiving bore and positioning the crown with its bottom face against a stop and one side of the cooling gallery against a locator; and
d. finish machining the combustion crater, the top face, the ring grooves, and the cylindrical outer surface of the side wall while the crown is so positioned.
2. The method, as set forth in claim 1, including the step of forging the crown from a billet of steel alloy to approximately the shape of the finished crown with sufficient material for the rough machining and finish machining steps.
3. The method, as set forth in claim 2, wherein the steel alloy is comprised of carbon, manganese, phosphorus, sulfur, silicon, chromium, molybdenum and the balance iron and trace elements.
4. The method, as set forth in claim 1, wherein approximately 0.030 inch (0.75 mm) of material remains after the rough machining step to be removed by the finish machining step.
5. The method, as set forth in claim 1, wherein the step of rough machining includes holding the crown by clamping the bosses in a chuck.
6. The method, as set forth in claim 1, wherein the step of rough machining includes:
a. grasping the side wall adjacent one end thereof and machining a portion of the outer cylindrical surface thereof between another end of the side wall and an area overlying the position of one of the ring grooves.
b. grasping said rough finished portion of the cylindrical outer surface, and rough machining the remaining portion of the cylindrical outer surface of the side wall between said one end and said overlying area of the one ring groove;
c. cutting said one ring groove in the side wall and removing any juncture of the rough machining operations of steps a and b; and
d cutting the remainder of said ring grooves.
7. The method, as set forth in claim 1, including the steps of:
a. rough machining the pin receiving bore in the bosses;
b. finish machining the pin receiving bore;
c. installing bushings in the finished bore; and
d. machining an inner diameter of the installed bushings to their finished diameter before step c of claim 1.
8. In a method of machining a crown of an articulated piston, the crown having a circular top face, a combustion crater extending from and below the top face, a relatively short side wall depending from the top face and having a cylindrical outer surface, a plurality of ring grooves recessed in the side wall and disposed at spaced locations below the top face, the side wall having an inner surface forming a first side of a cooling gallery that extends adjacent the top face and the combustion crater, a depending center section having a laterally-extending pin-receiving bore therethrough, the side wall having a bottom face extending between the cylindrical side wall and the cooling gallery and disposed above the pin-receiving bore, the method of machining comprising:
a. grasping the side wall adjacent one end thereof and rough finishing a portion of the cylindrical outer surface thereof between another end of the side wall and an area overlying the position of one of the ring grooves;
b. grasping said rough finished portion of the outer surface, and rough finishing another portion of the cylindrical outer surface of the side wall between said one end and said overlying area of the one ring groove;
c. cutting said one ring groove in the side wall and removing any juncture of the rough finishing operations of steps a and b; and
d. cutting the remainder of said ring grooves.
9. In a method of machining a crown of an articulated piston, as set forth in claim 8, further comprising the steps of:
a. rough machining the top face, the combustion crater and the bottom face;
b. finish machining the bottom face of the crown;
c. machining the laterally-extending pin-receiving bore through the depending center section;
d. inserting a member through the pin receiving bore and positioning the crown with the bottom face against a stop and one side of the cooling gallery against a locator; and
e. finish machining the combustion crater, the top face, the cylindrical outer surface and the ring grooves while the crown is so positioned.
US07261457 1988-10-21 1988-10-21 Method of producing a crown for an articulated piston Expired - Lifetime US4847964B1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US07261457 US4847964B1 (en) 1988-10-21 1988-10-21 Method of producing a crown for an articulated piston
PCT/US1988/004605 WO1990004491A1 (en) 1988-10-21 1988-12-23 A method of producing a crown for an articulated piston
JP1501366A JP2801049B2 (en) 1988-10-21 1988-12-23 Method of manufacturing a crown for an articulated piston
EP89901407A EP0439459B1 (en) 1988-10-21 1988-12-23 A method of producing a crown for an articulated piston
DE8989901407T DE3875253T2 (en) 1988-10-21 1988-12-23 METHOD FOR PRODUCING A HEADBOARD FOR A TWO-PIECE PISTON.
BR888807924A BR8807924A (en) 1988-10-21 1988-12-23 PROCESS FOR THE PRODUCTION OF A CROWN FOR ARTICULATED PLATE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07261457 US4847964B1 (en) 1988-10-21 1988-10-21 Method of producing a crown for an articulated piston

Publications (2)

Publication Number Publication Date
US4847964A true US4847964A (en) 1989-07-18
US4847964B1 US4847964B1 (en) 2000-05-09

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US (1) US4847964B1 (en)
EP (1) EP0439459B1 (en)
JP (1) JP2801049B2 (en)
BR (1) BR8807924A (en)
DE (1) DE3875253T2 (en)
WO (1) WO1990004491A1 (en)

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2667260A1 (en) * 1990-09-28 1992-04-03 Metal Leve Sa Method for the manufacture of a piston in two parts
US5150517A (en) * 1990-04-17 1992-09-29 Metal Leve S/A Industria E Comercio Method of manufacturing a piston
US5230148A (en) * 1990-04-20 1993-07-27 Metal Leve S/A Industria E Comercio Method for the manufacture of a cooled engine piston head
DE4446726A1 (en) * 1994-12-24 1996-06-27 Mahle Gmbh Process for producing a one-piece cooling channel piston
GB2297282A (en) * 1995-01-25 1996-07-31 T & N Technology Ltd Machining pistons
US5720101A (en) * 1995-09-25 1998-02-24 Teijin Seiki Boston, Inc Hermetically sealed harmonic drive transmission manufacture
US5839352A (en) * 1996-08-07 1998-11-24 Cummins Engine Company, Inc. Articulated piston
US6155157A (en) * 1998-10-06 2000-12-05 Caterpillar Inc. Method and apparatus for making a two piece unitary piston
WO2001063112A1 (en) * 2000-02-24 2001-08-30 Volkswagen Aktiengesellschaft Method for production of a piston for a reciprocating internal combustion engine
WO2001073275A1 (en) * 2000-03-28 2001-10-04 Federal-Mogul Corporation Heavy duty piston having oil splash deflector
US6487773B2 (en) * 2001-03-23 2002-12-03 Mahle Gmbh Method of making one-piece piston
US6494170B2 (en) 2000-12-01 2002-12-17 Caterpillar Inc Two-piece piston assembly with skirt having pin bore oil ducts
US20030150112A1 (en) * 2002-02-12 2003-08-14 Upadhya Srinivasa K. Piston machining
US6698078B2 (en) 2001-06-21 2004-03-02 American Axle & Manufacturing, Inc. Method for forming two piece axle shaft
US20080087450A1 (en) * 2006-10-11 2008-04-17 Trong-Ruey Lin Method for assembling a front cover to a bush in a pneumatic tool
WO2009068494A2 (en) * 2007-11-30 2009-06-04 Andreas Borst Piston and method for the production thereof
US20100329801A1 (en) * 2009-06-24 2010-12-30 Jiancheng Liang Method of forming piston pin holes and boring system therefor
DE10049786B4 (en) * 1999-10-07 2011-01-13 Cummins Inc., Columbus High temperature resistant material for split pistons
US20110030214A1 (en) * 2009-08-05 2011-02-10 Wolfgang Rein Piston assembly multiple step forming process
EP2301708A3 (en) * 2009-09-23 2012-11-21 Bayerische Motoren Werke Aktiengesellschaft Method for producing a roof profile of a combustion engine piston and combustion engine piston produced according to the method
US20130000120A1 (en) * 2009-09-04 2013-01-03 Mahle International Gmbh Method for producing an aluminum piston for an internal combustion engine
CN104646687A (en) * 2014-06-21 2015-05-27 柳州凯通机械有限公司 Aluminum piston machining method
CN112658596A (en) * 2020-11-16 2021-04-16 山东振挺精工活塞有限公司 Process for solving problem of unqualified parallelism of die-casting piston pin hole
DE102023109640A1 (en) 2022-04-27 2023-11-02 Caterpillar Inc. METHOD FOR PRODUCING PISTONS WITH POLISHING REMOVAL OF THERMAL INSULATING LAYER (WDS) MATERIAL

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US5150517A (en) * 1990-04-17 1992-09-29 Metal Leve S/A Industria E Comercio Method of manufacturing a piston
US5359922A (en) * 1990-04-17 1994-11-01 Metal Leve S/A Industria E Comercio Head of two welded parts for two-piece articulated piston
US5230148A (en) * 1990-04-20 1993-07-27 Metal Leve S/A Industria E Comercio Method for the manufacture of a cooled engine piston head
US5317958A (en) * 1990-04-20 1994-06-07 Metal Leve S/A Industria E Comercio Head for a two piece articulated piston
US5588351A (en) * 1990-09-28 1996-12-31 Metal Leve S/A Industria E Comercio Head for two piece articulated piston
US5245752A (en) * 1990-09-28 1993-09-21 Metal Leve S/A Industria E Comercio Method of manufacturing a two piece piston
FR2667260A1 (en) * 1990-09-28 1992-04-03 Metal Leve Sa Method for the manufacture of a piston in two parts
DE4446726A1 (en) * 1994-12-24 1996-06-27 Mahle Gmbh Process for producing a one-piece cooling channel piston
US5778533A (en) * 1994-12-24 1998-07-14 Mahle Gmbh Method of producing a one-part cooling duct piston
GB2297282A (en) * 1995-01-25 1996-07-31 T & N Technology Ltd Machining pistons
GB2297282B (en) * 1995-01-25 1997-07-23 T & N Technology Ltd Machining pistons
US5720101A (en) * 1995-09-25 1998-02-24 Teijin Seiki Boston, Inc Hermetically sealed harmonic drive transmission manufacture
US5839352A (en) * 1996-08-07 1998-11-24 Cummins Engine Company, Inc. Articulated piston
US6155157A (en) * 1998-10-06 2000-12-05 Caterpillar Inc. Method and apparatus for making a two piece unitary piston
DE10049786B4 (en) * 1999-10-07 2011-01-13 Cummins Inc., Columbus High temperature resistant material for split pistons
US6681485B2 (en) 2000-02-24 2004-01-27 Volkswagen Ag Method for casting a piston for a reciprocating internal combustion engine
WO2001063112A1 (en) * 2000-02-24 2001-08-30 Volkswagen Aktiengesellschaft Method for production of a piston for a reciprocating internal combustion engine
WO2001073275A1 (en) * 2000-03-28 2001-10-04 Federal-Mogul Corporation Heavy duty piston having oil splash deflector
US6371061B2 (en) 2000-03-28 2002-04-16 Federal-Mogul World Wide, Inc. Heavy duty piston having oil splash deflector and method of cooling a piston
US6494170B2 (en) 2000-12-01 2002-12-17 Caterpillar Inc Two-piece piston assembly with skirt having pin bore oil ducts
US6487773B2 (en) * 2001-03-23 2002-12-03 Mahle Gmbh Method of making one-piece piston
US6698078B2 (en) 2001-06-21 2004-03-02 American Axle & Manufacturing, Inc. Method for forming two piece axle shaft
US20030150112A1 (en) * 2002-02-12 2003-08-14 Upadhya Srinivasa K. Piston machining
US6760961B2 (en) * 2002-02-12 2004-07-13 Focus: Hope Piston machining
US20080087450A1 (en) * 2006-10-11 2008-04-17 Trong-Ruey Lin Method for assembling a front cover to a bush in a pneumatic tool
WO2009068494A3 (en) * 2007-11-30 2009-08-20 Andreas Borst Piston and method for the production thereof
WO2009068494A2 (en) * 2007-11-30 2009-06-04 Andreas Borst Piston and method for the production thereof
US20100329801A1 (en) * 2009-06-24 2010-12-30 Jiancheng Liang Method of forming piston pin holes and boring system therefor
US8506215B2 (en) 2009-06-24 2013-08-13 Federal-Mogul Corporation Method of forming piston pin holes and boring system therefor
US8926239B2 (en) 2009-06-24 2015-01-06 Federal-Mogul Corporation Method of forming piston pin holes and boring system therefor
US20110030214A1 (en) * 2009-08-05 2011-02-10 Wolfgang Rein Piston assembly multiple step forming process
US20130000120A1 (en) * 2009-09-04 2013-01-03 Mahle International Gmbh Method for producing an aluminum piston for an internal combustion engine
EP2301708A3 (en) * 2009-09-23 2012-11-21 Bayerische Motoren Werke Aktiengesellschaft Method for producing a roof profile of a combustion engine piston and combustion engine piston produced according to the method
CN104646687A (en) * 2014-06-21 2015-05-27 柳州凯通机械有限公司 Aluminum piston machining method
CN112658596A (en) * 2020-11-16 2021-04-16 山东振挺精工活塞有限公司 Process for solving problem of unqualified parallelism of die-casting piston pin hole
DE102023109640A1 (en) 2022-04-27 2023-11-02 Caterpillar Inc. METHOD FOR PRODUCING PISTONS WITH POLISHING REMOVAL OF THERMAL INSULATING LAYER (WDS) MATERIAL

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EP0439459A1 (en) 1991-08-07
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JPH04501087A (en) 1992-02-27
WO1990004491A1 (en) 1990-05-03
BR8807924A (en) 1991-08-13
US4847964B1 (en) 2000-05-09
JP2801049B2 (en) 1998-09-21
DE3875253D1 (en) 1992-11-12

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